What was found
FUSELAGE SKIN DAMAGE AT STA 600-660 STR 16L. CONSTANT THICKNESS SKIN WAS SPLICED INTO THE SKIN PANEL USING DOUBLER STRAPS AND TRIPLERS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN DAMAGE AT STA 600-660 STR 16L. CONSTANT THICKNESS SKIN WAS SPLICED INTO THE SKIN PANEL USING DOUBLER STRAPS AND TRIPLERS.